@inproceedings{92c9f511187d4ed9a16d40570c826e9f,
title = "One kind of flight control system design for separation section in cruise missile",
abstract = "Separation section is the most complex and dramatic stage in disturbing the cruise missile during the entire flight trajectory. The characteristic of low-altitude, low-speed, non-aileron flight separation of the missile propelled by rocket was analyzed in this paper. Classic engineering methods and neural network dynamic inversion methods was used to design control system, and two different control methods were compared.",
keywords = "Dynamic inversion, Flight control system, Missile patrol, Neural networks",
author = "Xiaodong Yuan and Shiqiao Gao",
year = "2012",
doi = "10.4028/www.scientific.net/AMR.490-495.885",
language = "English",
isbn = "9783037853849",
series = "Advanced Materials Research",
pages = "885--889",
booktitle = "Mechatronics and Intelligent Materials II",
note = "2nd International Conference on Mechatronics and Intelligent Materials 2012, MIM 2012 ; Conference date: 18-05-2012 Through 19-05-2012",
}